JPS59155577A - Blade of windmill - Google Patents
Blade of windmillInfo
- Publication number
- JPS59155577A JPS59155577A JP58029377A JP2937783A JPS59155577A JP S59155577 A JPS59155577 A JP S59155577A JP 58029377 A JP58029377 A JP 58029377A JP 2937783 A JP2937783 A JP 2937783A JP S59155577 A JPS59155577 A JP S59155577A
- Authority
- JP
- Japan
- Prior art keywords
- blade
- rotor
- poured
- foamed plastic
- filling
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000005452 bending Methods 0.000 claims abstract description 12
- 239000000057 synthetic resin Substances 0.000 abstract description 3
- 229920003002 synthetic resin Polymers 0.000 abstract description 3
- 239000000945 filler Substances 0.000 abstract 2
- 238000000034 method Methods 0.000 abstract 1
- 238000010586 diagram Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 238000010248 power generation Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 239000000088 plastic resin Substances 0.000 description 1
- 229920003217 poly(methylsilsesquioxane) Polymers 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/06—Rotors
- F03D1/065—Rotors characterised by their construction elements
- F03D1/0658—Arrangements for fixing wind-engaging parts to a hub
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
Abstract
Description
【発明の詳細な説明】 ものである。[Detailed description of the invention] It is something.
風ツノ発電に、風のエイ・ルキーを利用して電気工不ル
ギーを発生させる装置であるが、風の持つ工不ルキー密
１江が小さいため、水力あるいは火力発電に：咬べて、
発電浴液の割に設置１ｉ＃費がが力・るのが現状である
。This is a device that uses the energy of the wind to generate electric power, but since the energy of the wind is small, it can be used for hydropower or thermal power generation.
The current situation is that the installation cost is quite high considering the power generation bath liquid.
特に凧屯の場合に、叉の製作費が楢も大きな割合を占め
ている。このため、風車振銘として、既に生産（暇産）
されているベリコブターのロータ、牛〒に安１’＋ｌ［
ｉ Ｉｙこ人手できる中古品を採用し、設備費の低減を
計っている。Particularly in the case of kite kites, the production cost of the fork also accounts for a large portion of the cost. For this reason, the windmill is already in production (time production).
The rotor of the Bellycow pig, which has been
We aim to reduce equipment costs by using second-hand items that can be done by hand.
しかるに、ヘリコプター〇ロータの回転は、水平面内で
あり、かつ、その数例けに、フレキシブルルートとなっ
ているため、翼にかかる応力は、回転の遠・し・刀によ
る引張応力が主で、曲げ応力は、ほとんどかからない設
計となっている。However, since the rotor of a helicopter rotates in a horizontal plane and in a few cases has a flexible route, the stress applied to the wings is mainly tensile stress due to the distance of rotation. The design is such that almost no bending stress is applied.
しかし、このロータを風屯痙に使用した場合、喝の回転
に垂直面となるため、重力による繰り返しの曲げ応力が
力・かり、さらに粱取付部もリジツドとなるため、大き
な曲げ応力が発生する。However, when this rotor is used for wind turbines, the plane is perpendicular to the rotation of the rotor, so the repeated bending stress due to gravity becomes a force, and the rotor attachment part also becomes rigid, resulting in large bending stress. .
また、ヘリコプタのロータは、直噴を軽減するため、死
所面は空胴となっている。そのため、大きな曲は応力が
かかると、１坐屈か′主じ、中苧の翼断面が＠．変じ、
兄の破損につながる恐れがある。In addition, the rotor of a helicopter has a hollow dead surface to reduce direct injection. Therefore, when stress is applied to a large bend, the wing cross-section of the central ram will become ＠. change,
There is a risk that it may lead to damage to the older brother.
従って、ヘリコプタ−のロータを風車用の翼として使用
する場合には曲げ応力にｊ（１ｊ」えるための強化対策
が必要である。Therefore, when a helicopter rotor is used as a wind turbine blade, it is necessary to take measures to strengthen the rotor to reduce the bending stress by 1j.
本発明は、風車用翼として、安１曲な、１クリえ（ｒｉ
１６「１用年数を経過した使用済のヘリコプタ−用のロ
ータを使用し、更に翼内部に樹脂首たほ発泡プラスチッ
ク、来月、軽金属等の物質を充」填することにより、軽
晴、かつロータ１１本がイ１゛するフンキンビリティ全
損うこと無く、曲げ応力による１」４屈に対し１優れた
而」力を有することを特徴とする。The present invention can be used as a blade for a wind turbine.
16 ``Using a rotor for a used helicopter that has been in use for one year, and filling the inside of the wing with materials such as resin-necked foam plastic and next month, light metal, etc.'' The 11 rotors are characterized by having excellent strength against bending due to bending stress without completely losing the strength of the rotor.
本発明に、風東用翼としてヘリコプタのロータを用いた
場合、強度上の不安点を取り除き、粱としての信頼件向
十を言するものである。In the present invention, when a helicopter rotor is used as a wing for use in the wind direction, concerns about strength are eliminated, and the reliability of the rotor is improved.
第一図ないし第１図に示すとおり、シ唱げブｌ／ −ド
カ７／、ブレードスパー−、リーマボルト３、絶、１禄
体（電食防止用）！ｉ、乙、フより構成される。As shown in Figures 1 and 1, there is a blade spar, a reamer bolt 3, a reamer bolt, and a 1-roku body (for preventing electrolytic corrosion). Consists of i, otsu, and f.
発泡グラスナックまたは合成樹脂等の充填拐ｑけｔ主人
１コ１０より注入され、翼内部の仝胴に充」値する。こ
の充填範囲は翼全長に亘る場合もあるが、応力が大きく
なる翼根近傍に限定する場合もある。Filling material such as foamed glass or synthetic resin is injected into the main body 10 and filled into the body inside the wing. This filling range may span the entire length of the blade, but may also be limited to the vicinity of the blade root where stress is high.
寸た。、＋ｑＨ艮都に硬質の発？包プラスチックを、殻
先’；”ｌ＜部に悼軟質の発泡プラスチックを注入する
ことにより、ロータ自体の有する７レキ／ビリテイを出
来るたけ川なわないように配ｌ促することも荷動である
。Dimensions. , +qH A hard release from Ato? By injecting soft foamed plastic into the tip of the shell, it is also possible to arrange the rotor's strength so that it does not bend as much as possible. .
ＭｉＪ ’ｇ己免に、フ゛レードカフｌにより連結’ｌ
’ｌｌ＋ ｇにホ゛ルト９で読１Ｍ月けられる。Connected to MiJ'g Self-Immunity by a field cuff.
'll+g was read in holt 9 for 1M months.
本発明による風車荻は、従来の中空翼に比べて、津屈荷
屯 約／、３ 倍
塵屑変位 約３．／ ３倍
の耐性を有する（下記表、風車４べの１牟屈試験結果参
照）。The wind turbine shaft according to the present invention has a dust displacement of about 3 times as much as a conventional hollow blade. / 3 times more durable (see table below, wind turbine 4/1 bending test results).
なお、ロータ仝胴部への充ＪＪ拐旧としては前記の発泡
プラスチックまたげ合成樹脂の他に不利系、軽金属等も
利用ｉｉｌ’能である。In addition to the above-mentioned foamed plastic and synthetic resin, it is also possible to use unfavorable materials, light metals, etc. to fill the rotor body.
以上説明した本発明の翼によると窒胴部に充填利ヲ充填
し曲げ応力に対する１１１Ｈ性を・伺与しているので、
強度−ヒの不安点全解消することができ、翼としてのイ
ト頁１′」二の向」二を言することかできる。According to the blade of the present invention as described above, the nitrogen body is filled with a filling effect and exhibits 111H resistance against bending stress.
All of the concerns about strength can be resolved, and it can be said that it will act as a wing.
第１図（は翼の乎面図、第２図は第１図のＡ部詳細断面
図、第３図げ第１図のＢ部詳細断面図、第４図は第Ω図
のＣ−Ｃ線矢硯の断面図、第Ｓ図は第３図の１．） −
Ｄ脚矢硯の断面図、第６図は１坐屈変位についての荷重
略図、第７図に従来品の１里屈の形で凹形企示す略図、
第８図は本発明翼の１坐）ｉシの形で凸形を示す略図で
ある。
／・・ブレードカフ、λ・・ブレードカフく−、３・・
リーマボルト、Ｕ−・充填ｌ’４’ｉ 、ｙ、 ｘ
、 ７・ ・ 絶ヒ及１本、 ８ ・ ・ １車結
ｌｌ１１１１１９ ・ ・ ホ ル １・ 、 ／
０・・注入［］。Figure 1 (is a plan view of the wing, Figure 2 is a detailed sectional view of section A in Figure 1, Figure 3 is a detailed sectional view of section B in Figure 1, and Figure 4 is a detailed sectional view of section B in Figure 1. A cross-sectional view of the line arrow inkstone, Figure S is 1.) in Figure 3.
A cross-sectional view of the D-leg arrow inkstone, FIG. 6 is a schematic diagram of the load for one bending displacement, and FIG. 7 is a schematic diagram showing the concave shape of the conventional product with one bending.
FIG. 8 is a schematic diagram showing the convex shape of the wing of the present invention. /...Blade cuff, λ...Blade cuff, 3...
Reamer bolt, U-・Filling l'4'i, y, x
, 7. ・ 1 connection, 8. ・ 1 car connection ll111119 ・ . Hole 1. , /
0... Injection [].
Claims (1)
に曲げ応力によって発生する座屈にズづする］１１１−
ｊ１１゛を改善するため充填刊全充填したことを％徴と
する風屯翼。Using a helicopter rotor, the buckling caused by bending stress in the 9th barrel of the 1st vine of the core rotor is investigated] 111-
In order to improve j11゛, the wind ton wing is a percentage sign that it is fully filled.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP58029377A JPS59155577A (en) | 1983-02-25 | 1983-02-25 | Blade of windmill |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP58029377A JPS59155577A (en) | 1983-02-25 | 1983-02-25 | Blade of windmill |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS59155577A true JPS59155577A (en) | 1984-09-04 |
Family
ID=12274453
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP58029377A Pending JPS59155577A (en) | 1983-02-25 | 1983-02-25 | Blade of windmill |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS59155577A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6420353U (en) * | 1987-07-29 | 1989-02-01 | ||
| GB2436598A (en) * | 2006-03-30 | 2007-10-03 | Boost Energy Systems Ltd | Wind turbine blade mounting |
| KR100813657B1 (en) | 2006-08-21 | 2008-03-18 | 원인호 | Sunlight Wheel Multi-Wind Windmill |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS569672A (en) * | 1979-06-21 | 1981-01-31 | Budd Co | Windmill blade structure and making method thereof |
| JPS57210171A (en) * | 1981-04-01 | 1982-12-23 | Messerschmitt Boelkow Blohm | Aerodynamical large-sized blade, particularly, rotor blade for large-sized air force device |
-
1983
- 1983-02-25 JP JP58029377A patent/JPS59155577A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS569672A (en) * | 1979-06-21 | 1981-01-31 | Budd Co | Windmill blade structure and making method thereof |
| JPS57210171A (en) * | 1981-04-01 | 1982-12-23 | Messerschmitt Boelkow Blohm | Aerodynamical large-sized blade, particularly, rotor blade for large-sized air force device |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6420353U (en) * | 1987-07-29 | 1989-02-01 | ||
| GB2436598A (en) * | 2006-03-30 | 2007-10-03 | Boost Energy Systems Ltd | Wind turbine blade mounting |
| KR100813657B1 (en) | 2006-08-21 | 2008-03-18 | 원인호 | Sunlight Wheel Multi-Wind Windmill |
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